VNE (S.L.)

281

km/h

152

kts

Max Speed (S.L.)

267

km/h

144

kts

Hovering IGE

4450

m

14600

ft

Hovering OGE

3261

m

10700

ft

Service ceiling

>6096

m

>20000

ft

Max Range (1)

991

km

535

NM

Max endurance (1)

†

(1) with 230 USGal fuel, no reserve, @ 5000 ft.

Weights

Max take Off (int./ loads)

2720

kg

5997

lb

Max take Off (ext./ loads)

3150

kg

6944

lb

Basic Empty Weights

1430

kg

3152

lb

Engine Rating (Pratt & Whitney PT6B-37A)

Take Off

747

kW

1002

SHP

Maximum continuous

650

kW

872

SHP

Transmission Rating

Take Off

671

kW

900

SHP

Max continuous

671

kW

900

SHP

Fuel Capacity

3 cell fuel system

605

l

160

USG

4 cell fuel system

710

l

188

USG

5 cell fuel system

870

l

230

USG

Crew

Pilot / Passengers

1 / 7

†

External Dimensions

Length (rotors turning)

13,01

m

42,68

ft

Width (rotor blades at 45∞)

7,66

m

25,13

ft

Maximum height

3,77

m

12,37

ft

Main rotor diameter

10,83

m

35,53

ft

Tail rotor diameter

2,00

m

6,57

ft

MR tip blade ground clearance

2,54

m

8,33

ft

TR tip blade ground clearance

1,29

m

4,23

ft

Fuselage ground clearance

0,54

m

1,77

ft

Performance (ISA, 2550 kg / 5622 lb)